A geometric controller based on dynamic feedback linearization achieves almost-global asymptotic stability for attitude tracking on a novel underactuated swiveling biplane-quadrotor tailsitter.
Systematic design methodology for development and flight testing of a variable pitch quadrotor biplane vtol uav for payload delivery .Mecha- tronics, 55:94–114, 2018
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Attitude Control of a Novel Tailsitter: Swiveling Biplane-Quadrotor
A geometric controller based on dynamic feedback linearization achieves almost-global asymptotic stability for attitude tracking on a novel underactuated swiveling biplane-quadrotor tailsitter.